EP0295295A1 - Process for data transmission by means of a geo-stationary satellite and at least one sub-satellite - Google Patents

Process for data transmission by means of a geo-stationary satellite and at least one sub-satellite

Info

Publication number
EP0295295A1
EP0295295A1 EP88900949A EP88900949A EP0295295A1 EP 0295295 A1 EP0295295 A1 EP 0295295A1 EP 88900949 A EP88900949 A EP 88900949A EP 88900949 A EP88900949 A EP 88900949A EP 0295295 A1 EP0295295 A1 EP 0295295A1
Authority
EP
European Patent Office
Prior art keywords
satellite
satellites
transmission
sub
earth
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
EP88900949A
Other languages
German (de)
French (fr)
Inventor
Manfred Schukat
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of EP0295295A1 publication Critical patent/EP0295295A1/en
Ceased legal-status Critical Current

Links

Classifications

    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04B—TRANSMISSION
    • H04B7/00—Radio transmission systems, i.e. using radiation field
    • H04B7/14—Relay systems
    • H04B7/15—Active relay systems
    • H04B7/185—Space-based or airborne stations; Stations for satellite systems
    • H04B7/195—Non-synchronous stations
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04B—TRANSMISSION
    • H04B7/00—Radio transmission systems, i.e. using radiation field
    • H04B7/14—Relay systems
    • H04B7/15—Active relay systems
    • H04B7/185—Space-based or airborne stations; Stations for satellite systems
    • H04B7/1851—Systems using a satellite or space-based relay
    • H04B7/18513—Transmission in a satellite or space-based system
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L23/00—Apparatus or local circuits for systems other than those covered by groups H04L15/00 - H04L21/00
    • H04L23/02—Apparatus or local circuits for systems other than those covered by groups H04L15/00 - H04L21/00 adapted for orthogonal signalling
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04B—TRANSMISSION
    • H04B7/00—Radio transmission systems, i.e. using radiation field
    • H04B7/14—Relay systems
    • H04B7/15—Active relay systems
    • H04B7/185—Space-based or airborne stations; Stations for satellite systems
    • H04B7/19—Earth-synchronous stations

Definitions

  • the invention relates to a method for transmitting data by means of a geostationary satellite and at least one sub-satellite, the sub-satellites being in lower orbits.
  • Communication satellites generally describe a geostationary orbit at a height of approximately 36,000 km above the equator. There they have a fixed orbit position, so that the same transmission frequency can be used for each satellite due to the distance between two neighboring satellites. As the geostationary orbit fills up slowly, other satellite orbits are planned, e.g. Subsatellite orbits with a height of a few hundred km or so-called quasi-stationary orbits. More details are e.g. the reference
  • this is achieved in that at least two data streams of the same frequency with different power / Hz are used for message transmission, the first data stream with higher power / Hz being used for connection to the geostationary satellite and the further data streams by means of PN (pseudo-noise) sequences are transmitted and serve to connect with the subsatellites.
  • PN pseudo-noise
  • 1 schematically shows the arrangement of the satellite orbits and the range of interference during transmission with the same frequency f ß ,
  • FIG. 3b shows the conditions in the transponder of the geostationary satellite with reception of the interference power.
  • Figure 1 shows schematically the arrangement of the satellite orbits.
  • the communications satellite S is located on a geostationary orbit at a distance of approximately 36,000 km, and the subsatellite S 2 on a subsatellite orbit at a distance of approximately 400 km - the former receives data from an earth station E, and the latter from another Earth station E ⁇ .
  • there is an interference area in which the two cones of the transmitting antennas overlap For this reason, as mentioned at the beginning, it is not readily possible to use the same frequencies for the two earth stations.
  • the structure of the PN sequences is constructed according to FIG 2 is that they have good correlation properties, which enables an exact De 'tetechnisch of Sig ⁇ Nals possible.
  • Each data bit is spread over the length of a PN sequence. If the length of the PN sequence is 1000 chips, for example, a data bit is represented by these 1000 chips.
  • the power per Hz to be applied in this way is therefore only 1/1000 of the power required in conventional methods. Both data streams are therefore decoupled from one another by a factor of 1000 in terms of their performance.
  • the transmissible useful bit rate is reduced by the factor of the spread compared to the conventional data stream by spreading the transmission spectrum, ie by using PN sequences.
  • PN sequences ie by using PN sequences.
  • a communication link with the same transmission frequency of 14 GHz is to be set up via a satellite S 2 , which is in a different orbit, for example in a circular orbit of lower height or an elliptical orbit.
  • the antenna may cover a certain area of the geostationary orbit on which the other satellite S is located and disrupts its message transmissions.
  • the ground station E now transmit according to FIG. 3a with a bandwidth of 10 MHz to the geostationary satellite S, and the ground station E 2 with the same bandwidth to the sub-satellite S 2 - but for transmission it uses PN sequences with a spreading factor of 1 1000 '.
  • the ground station E 2 can only transmit a useful bit rate of approx. 10 K bits compared to the 10 M bits of the ground station E,.
  • the transmission power required for the 10 KBits is distributed over 10 MHz, so that within the 10 MHz bandwidth of the geostationary satellite S-, its own signal is only disturbed by a factor of 1/1000. According to FIG. 3b, only the background noise of the transponder is increased.
  • +20 is steamed about 10.
  • Particularly expedient applications of the invention consist in that the additional data streams transmit information for controlling and / or regulating the message traffic between satellite-satellite and / or earth-satellite-earth or for controlling and / or regulating the satellites with respect to their orbit become.

Landscapes

  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Signal Processing (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Radio Relay Systems (AREA)

Abstract

Dans le procédé décrit les satellites secondaires sont placés sur des orbites plus basses. Pour la transmission des communications, on utilise au moins deux flux de données de différentes puissances/Hz, le premier flux, à puissance plus forte/Hz étant utilisé pour assurer la liaison avec le satellite géostationnaire (S1) et les autres flux étant transmis au moyen de séquences de bruits aléatoires. Deux transmissions de données ont ainsi lieu dans la même gamme de fréquences, par utilisation toutefois de deux satellites différents qui se trouvent à portée de vue d'une station terrestre. Une application particulièrement adéquate de l'invention est la transmission par flux de données appropriée des informations nécessaires au contrôle et/ou à la régulation de l'échange de communications d'un satellite à l'autre et/ou par les voies terre-satellite-terre ou pour contrôler ou régler l'orbite des satellites.In the process described, the secondary satellites are placed in lower orbits. For the transmission of communications, at least two data streams of different powers / Hz are used, the first stream, at higher power / Hz, being used to provide the link with the geostationary satellite (S1) and the other streams being transmitted to the using random noise sequences. Two data transmissions thus take place in the same frequency range, however by the use of two different satellites which are within sight of a ground station. A particularly suitable application of the invention is the transmission by appropriate data flow of the information necessary for controlling and / or regulating the exchange of communications from one satellite to another and / or by the earth-satellite channels. - earth or to control or adjust the orbit of the satellites.

Description

Verfahren zur Übertragung von Daten mittels eines geostationären Satel¬ liten und wenigstens eines Subsatelliten. Method for the transmission of data by means of a geostationary satellite and at least one sub-satellite.
Die Erfindung betrifft ein Verfahren zur Übertragung von Daten mittels eines geostationären Satelliten und wenigstens eines Subsatelliten, wo¬ bei die Subsatelliten sich auf niedrigeren Umlaufbahnen befinden.The invention relates to a method for transmitting data by means of a geostationary satellite and at least one sub-satellite, the sub-satellites being in lower orbits.
Nachrichtensatelliten beschreiben im allgemeinen eine geostationare Kreisbahn in ca. 36000 km Höhe über dem Äquator. Dort haben sie eine fest zugeteilte Orbitposition, so daß für jeden Satelliten die gleiche Übertragungsfrequenz aufgrund der Entfernung zwischen zwei benachbarten Satelliten benutzt werden kann. Da sich der geostationare Orbit langsam füllt, werden andere Satellitenbahnen geplant, wie z.B. Subsatelliten- bahnen mit einer Höhe von einigen hundert km oder sogenannte quasistati¬ onäre Bahnen. Näheres dazu ist z.B. der LiteraturstelleCommunication satellites generally describe a geostationary orbit at a height of approximately 36,000 km above the equator. There they have a fixed orbit position, so that the same transmission frequency can be used for each satellite due to the distance between two neighboring satellites. As the geostationary orbit fills up slowly, other satellite orbits are planned, e.g. Subsatellite orbits with a height of a few hundred km or so-called quasi-stationary orbits. More details are e.g. the reference
P. Dondl : "LOOPUS erschließt dem Satellitenfunk eine neue Dimen¬ sion"; NTZ-Archiv Band 5 (1983), Heft 12, S. 327 - 335P. Dondl: "LOOPUS opens up a new dimension for satellite radio"; NTZ Archives Volume 5 (1983), No. 12, pp. 327 - 335
zu entnehmen.refer to.
Der gravierendste Nachteil dabei ist, daß unterschiedliche Frequenzbe¬ reiche verwendet werden müssen, um gegenseitige Störungen auszuschlie¬ ßen. Mit herkömmlichen Übertragungsverfahren ist es nämlich nicht ohne weiteres möglich, die gleiche Frequenz für den geostationären Satelliten und den Subsatelliten zu verwenden, da dadurch der geostationare Satel¬ lit gestört würde, zumal da Satelliten mit niedrigeren Bahnen während ihrer Sichtbarkeit mehrere geostation re Satelliten (bezogen auf die Abstrahlrichtung der Sende-Erdfunkstelle) , die ggf. das gleiche Fre¬ quenzband benutzen, passieren. Frequenzbereiche bzw. Übertragungs¬ bandbreiten sind jedoch international streng reglementiert und auf- geteilt, so daß sie nicht ohne weiteres verwendet werden können. Um den zukünftigen Bedarf an Kommunikation zu decken, müssen also zusätzliche Möglichkeiten geschaffen werden.The most serious disadvantage is that different frequency ranges have to be used in order to exclude mutual interference. With conventional transmission methods, it is not readily possible to use the same frequency for the geostationary satellite and the sub-satellite, since this would interfere with the geostationary satellite, especially since satellites with lower orbits have several geostationable satellites during their visibility (based on the direction of radiation of the transmitting earth station), which may use the same frequency band. However, frequency ranges and transmission bandwidths are strictly regulated internationally and divided so that they cannot be used easily. In order to meet the future need for communication, additional options must be created.
Es ist das Ziel der Erfindung, ein Verfahren der eingangs genannten Art zu schaffen, das es ermöglicht, mit den augenblicklichen (oder: vorgege¬ benen) Frequenzbereichen auszukommen.It is the aim of the invention to create a method of the type mentioned at the beginning which makes it possible to get by with the instantaneous (or: specified) frequency ranges.
Gemäß der Erfindung wird dies dadurch erreicht, daß zur Nachrichten¬ übertragung wenigstens zwei in ihrer Leistung/Hz unterschiedliche Daten¬ ströme gleicher Frequenz verwendet werden, wobei der erste Datenstrom mit höherer Leistung/Hz zur Verbindung mit dem geostationären Satelliten dient und die weiteren Datenströme mittels PN(Pseudo-Noise)-Folgen über¬ tragen werden und der Verbindung mit den Subsatelliten dienen.According to the invention, this is achieved in that at least two data streams of the same frequency with different power / Hz are used for message transmission, the first data stream with higher power / Hz being used for connection to the geostationary satellite and the further data streams by means of PN (pseudo-noise) sequences are transmitted and serve to connect with the subsatellites.
Es finden somit zwei Datenübertragungen im gleichen Frequenzbereich statt, wobei jedoch unterschiedliche Satelliten bedient werden.There are thus two data transmissions in the same frequency range, but different satellites are served.
Einzelheiten der Erfindung ergeben sich aus den Unteransprüchen und der Beschreibung, in der anhand der Zeichnung ein Ausführungsbeispiel erör¬ tert wird. Es zeigenDetails of the invention emerge from the subclaims and the description in which an exemplary embodiment is discussed with reference to the drawing. Show it
Fig. 1 schematisch die Anordnung der Satellitenbahnen und den Bereich der Störungen bei Übertragung mit der gleichen Frequenz fß,1 schematically shows the arrangement of the satellite orbits and the range of interference during transmission with the same frequency f ß ,
Fig. 2 schematisch das Prinzip der Spreizung mittels PN-Folgen,2 schematically shows the principle of spreading by means of PN sequences,
Fig. 3a die Verhältnisse im Transponder des geostationären Satelliten ohne Empfang der Störleistung undFig. 3a, the conditions in the transponder of the geostationary satellite without receiving the interference power and
Fig. 3b die Verhältnisse im Transponder des geostationären Satelliten mit Empfang der Störleistung. Figur 1 zeigt schematisch die Anordnung der Satellitenbahnen. Auf einer geostationären Bahn im Abstand von ca. 36 000 km Höhe befindet sich der Nachrichtensatellit S, und auf einer Subsatellitenbahn im Abstand von etwa 400 km Höhe der Subsatellit S2- Der erstere empfängt Daten von einer Erdstation E, , der letztere von einer weiteren Erdstation E~. Wie der Figur zu entnehmen ist, ergibt sich ein Störungsbereich, in dem sich die beiden Kegel der Sendeantennen überschneiden. Aus diesem Grunde ist es, wie eingangs erwähnt, nicht ohne weiteres möglich, gleiche Frequenzen für die beiden Erdstationen zu verwenden.3b shows the conditions in the transponder of the geostationary satellite with reception of the interference power. Figure 1 shows schematically the arrangement of the satellite orbits. The communications satellite S is located on a geostationary orbit at a distance of approximately 36,000 km, and the subsatellite S 2 on a subsatellite orbit at a distance of approximately 400 km - the former receives data from an earth station E, and the latter from another Earth station E ~. As can be seen in the figure, there is an interference area in which the two cones of the transmitting antennas overlap. For this reason, as mentioned at the beginning, it is not readily possible to use the same frequencies for the two earth stations.
Gemäß der Erfindung wird dies jedoch dadurch ermöglicht, daß zwei in ihrer Leistung/Hz unterschiedliche Datenströme gleicher Frequenz benutzt werden, wobei der erste Datenstrom mit höherer Leistung/Hz zur Verbin¬ dung mit dem geostationären Satelliten (S,) dient und die weiteren Datenströme mittels PN(Pseudo-Noise)-Folgen übertragen werden und der Verbindung mit den Subsatelliten (S~) dienen.According to the invention, however, this is made possible by using two data streams of the same frequency which have different power / Hz, the first data stream with higher power / Hz being used for connection to the geostationary satellite (S,) and the further data streams by means of PN (pseudo-noise) sequences are transmitted and serve to connect to the subsatellites (S ~).
Durch die leistungsmäßige Entkopplung beider Satellitensysteme kann der gleiche Frequenzbereich benutzt werden, ohne nennenswerte Störungen hervorzurufen.By decoupling the performance of both satellite systems, the same frequency range can be used without causing any significant interference.
Die Struktur der PN-Folgen ist gemäß Figur 2 so aufgebaut, daß sie gute Korrelationseigenschaften besitzen, was eine exakte De'tektion des Sig¬ nals ermöglicht. Jedes Datenbit wird dabei auf die Länge einer PN-Folge gespreizt. Beträgt die Länge der PN-Folge z.B. 1000 Chips, so wird ein Datenbit durch eben diese 1000 Chips dargestellt. Die so aufzubringende Leistung pro Hz beträgt demnach nur 1/1000 der Leistung, die bei konven¬ tionellen Verfahren erforderlich ist. Beide Datenströme sind also bezüg¬ lich ihrer Leistungum den Faktor 1000 voneinander entkoppelt.The structure of the PN sequences is constructed according to FIG 2 is that they have good correlation properties, which enables an exact De 'tektion of Sig¬ Nals possible. Each data bit is spread over the length of a PN sequence. If the length of the PN sequence is 1000 chips, for example, a data bit is represented by these 1000 chips. The power per Hz to be applied in this way is therefore only 1/1000 of the power required in conventional methods. Both data streams are therefore decoupled from one another by a factor of 1000 in terms of their performance.
Werden gleiche Bandbreiten benutzt, so reduziert sich durch Spreizung des Sendespektrums, d.h. durch Verwendung von PN-Folgen die übertragbare Nutzbitrate um den Faktor der Spreizung gegenüber dem konventionellen Datenstrom. Im folgenden wird davon ausgegangen, daß eine Nachrichtenverbindung zwi¬ schen Bodenstationen und einem geostationären Satelliten S^ (z.B. ECS) im 14-GHz-Bereich besteht.If the same bandwidths are used, the transmissible useful bit rate is reduced by the factor of the spread compared to the conventional data stream by spreading the transmission spectrum, ie by using PN sequences. In the following it is assumed that there is a communication link between ground stations and a geostationary satellite S ^ (eg ECS) in the 14 GHz range.
Jetzt soll zusätzlich eine Nachrichtenverbindung mit der gleichen Sende¬ frequenz von 14 GHz über einen Satelliten S2 aufgebaut werden, der sich in einer anderen Bahn befindet, z.B. in einer Kreisbahn geringerer Höhe oder einer elliptischen Bahn.Now, in addition, a communication link with the same transmission frequency of 14 GHz is to be set up via a satellite S 2 , which is in a different orbit, for example in a circular orbit of lower height or an elliptical orbit.
Aufgrund der niedrigeren Höhe des Subsatelliten S„ ist sein Sichtbar¬ keitsbereich für eine Bodenstation E2 beschränkt; d.h. pro Umlauf sieht ihn die Bodenstation E2 für 'n' Minuten. Sie muß den Satelliten S2 mit ihrer Antenne am aufgehenden Horizont erfassen und bis zum un¬ tergehenden Horizont verfolgen. Dadurch überstreicht die Antenne unter Umständen einen bestimmten Bereich der geostationären Bahn, auf dem sich der andere Satellit S, befindet und stört dessen Nachrichtenüber¬ tragungen.Due to the lower height of the subsatellite S ", its visibility range for a ground station E 2 is limited; ie the ground station E 2 sees it for 'n' minutes per revolution. It must detect the satellite S 2 with its antenna on the rising horizon and track it down to the setting horizon. As a result, the antenna may cover a certain area of the geostationary orbit on which the other satellite S is located and disrupts its message transmissions.
Die Bodenstation E, sende nun gemäß Figur 3a mit einer Bandbreite von 10 MHz zum geostationären Satelliten S, und die Bodenstation E2 mit der gleichen Bandbreite zum Subsatelliten S2- Zur Übertragung verwen¬ det sie aber PN-Folgen mit einem Spreizfaktor von l1000'.The ground station E, now transmit according to FIG. 3a with a bandwidth of 10 MHz to the geostationary satellite S, and the ground station E 2 with the same bandwidth to the sub-satellite S 2 - but for transmission it uses PN sequences with a spreading factor of 1 1000 '.
Da der Spreizfaktor das Verhältnis von Länge der PN-Folge zur Dauer ei¬ nes Datenbits angibt, kann die Bodenstation E2 nur eine Nutzbitrate von ca. 10 KBits gegenüber den 10 MBits der Bodenstation E, übertra¬ gen. Die notwendige Übertragungsleistung für die 10 KBits wird aber auf 10 MHz verteilt, so daß innerhalb der 10 MHz Bandbreite des geostationä¬ ren Satelliten S-, dessen eigenes Signal nur um den Faktor 1/1000 gestört wird. Es wird also gemäß Figur 3b lediglich das Grundrauschen des Trans- ponders erhöht.Since the spreading factor indicates the ratio of the length of the PN sequence to the duration of a data bit, the ground station E 2 can only transmit a useful bit rate of approx. 10 K bits compared to the 10 M bits of the ground station E,. The transmission power required for the 10 However, KBits is distributed over 10 MHz, so that within the 10 MHz bandwidth of the geostationary satellite S-, its own signal is only disturbed by a factor of 1/1000. According to FIG. 3b, only the background noise of the transponder is increased.
Es finden somit zwei Datenübertragungen im gleichen Frequenzbereich statt, wobei jedoch unterschiedliche Satelliten bedient werden, die sich beide im Sichtbarkeitsbereich der Erdstation E2 befinden. Die in Figur 3 gezeigten Leistungsverhältnisse würden nur dann gelten, wenn beide Satelliten die gleiche Höhe hätten. Da der Subsatellit S2 aber eine geringere Höhe benutzt, muß auch entsprechend weniger Leistung abgestrahlt werden. Das reduziert die in Figur 3b dargestellte vom geo¬ stationären Satelliten empfangene Störleistung noch weiter, zumal dieseTwo data transmissions therefore take place in the same frequency range, but different satellites are operated, both of which are located in the visibility range of the earth station E 2 . The power ratios shown in FIG. 3 would only apply if both satellites were at the same height. However, since the subsatellite S 2 uses a lower height, less power has to be emitted. This further reduces the interference power shown in FIG. 3b received by the geo-stationary satellite, especially since this
Störleistung aufgrund der Strahlenreduktion generell um den Faktor vonInterference due to radiation reduction generally by a factor of
+20 ca. 10 gedämpft wird.+20 is steamed about 10.
Besonders zweckmäßige Anwendungen der Erfindung bestehen darin, daß mit¬ tels der zusätzlichen Datenströme Informationen zum Steuern und/oder Regeln des Nachrichtenverkehrs zwischen Satellit-Satellit und /oder Erde-Satellit-Erde bzw. zum Steuern und/oder Regeln der Satelliten bezüglich ihrer Bahn übertragen werden. Particularly expedient applications of the invention consist in that the additional data streams transmit information for controlling and / or regulating the message traffic between satellite-satellite and / or earth-satellite-earth or for controlling and / or regulating the satellites with respect to their orbit become.

Claims

Patentansprüche: Claims:
1. Verfahren zur Übertragung von Daten mittels eines geostationären Satelliten und wenigstens eines Subsatelliten, wobei die Subsatelliten sich auf niedrigeren Umlaufbahnen befinden, d a d u r c h g e ¬ k e n n z e i c h n e , d a ß zur Nachrichtenübertragung wenigstens zwei in ihrer Leistung/Hz unterschiedliche Datenströme gleicher Frequenz verwendet werden, wobei der erste Datenstrom mit höherer Leistung/Hz zur Verbindung mit dem geostationären Satelliten (S,) dient und die weite¬ ren Datenströme mittels PN(Pseudo-Noise)-Folgen übertragen werden und der Verbindung mit den Subsatelliten (S2) dienen.1. Method for the transmission of data by means of a geostationary satellite and at least one sub-satellite, the sub-satellites being in lower orbits, characterized in that at least two different data streams of the same frequency are used for message transmission, the first Data stream with higher power / Hz is used to connect to the geostationary satellite (S,) and the further data streams are transmitted by means of PN (pseudo-noise) sequences and serve to connect to the subsatellites (S 2 ).
2. Verfahren nach Anspruch 1, d a d u r c h g e k e n n ¬ z e i c h n e t, d a ß mittels der weiteren Datenströme Informationen2. The method according to claim 1, d a d u r c h g e k e n n ¬ z e i c h n e t, d a ß by means of the further data streams information
"zum Steuern und/oder Regeln des Nachrichtenverkehrs zwischen Satellit- Satellit und /oder Erde-Satellit-Erde übertragen werden. " for controlling and / or regulating the communication between satellite-satellite and / or earth-satellite-earth are transmitted.
3. Verfahren nach Anspruch 1, d a d u r c h g e k e n n ¬ z e i c h n e t, d a ß mittels der weiteren Datenströme Informationen zum Steuern und/oder Regeln der Satelliten bezüglich ihrer Bahn über¬ tragen werden. 3. The method according to claim 1, d a d u r c h g e k e n n ¬ z e i c h n e t d a ß by means of the further data streams information for controlling and / or regulating the satellites are transmitted with respect to their orbit.
EP88900949A 1986-12-23 1987-12-19 Process for data transmission by means of a geo-stationary satellite and at least one sub-satellite Ceased EP0295295A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19863644176 DE3644176A1 (en) 1986-12-23 1986-12-23 METHOD FOR TRANSMITTING DATA BY MEANS OF A GEOSTATIONAL SATELLITE AND AT LEAST A SUBSATELLITE
DE3644176 1986-12-23

Publications (1)

Publication Number Publication Date
EP0295295A1 true EP0295295A1 (en) 1988-12-21

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EP88900949A Ceased EP0295295A1 (en) 1986-12-23 1987-12-19 Process for data transmission by means of a geo-stationary satellite and at least one sub-satellite

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US (1) US4985706A (en)
EP (1) EP0295295A1 (en)
AU (1) AU607738B2 (en)
DE (1) DE3644176A1 (en)
WO (1) WO1988004866A1 (en)

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AU1152388A (en) 1988-07-15
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DE3644176C2 (en) 1989-04-06
WO1988004866A1 (en) 1988-06-30

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